Design guidelines for the prevention of skin-stiffener debonding in composite aircraft panels
Design guidelines for the prevention of skin-stiffener debonding in composite aircraft panels
| dc.contributor.author | Rijn, J.C.F.N. van | en_US |
| dc.date.accessioned | 2013-10-30T12:53:03Z | |
| dc.date.available | 2013-10-30T12:53:03Z | |
| dc.date.issued | 2000 | en_US |
| dc.identifier.other | NLR-TP-2000-355 | en_US |
| dc.identifier.uri | http://hdl.handle.net/10921/849 | |
| dc.language.iso | en | en_US |
| dc.publisher | National Aerospace Laboratory NLR | en_US |
| dc.relation.ispartofseries | NLR Technical Publication;2000-355 | en_US |
| dc.subject.other | Composite materials | en_US |
| dc.subject.other | Structural stability | en_US |
| dc.title | Design guidelines for the prevention of skin-stiffener debonding in composite aircraft panels | en_US |
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